US4661953A - Error tracking apparatus in a data processing system - Google Patents

Error tracking apparatus in a data processing system Download PDF

Info

Publication number
US4661953A
US4661953A US06/907,131 US90713186A US4661953A US 4661953 A US4661953 A US 4661953A US 90713186 A US90713186 A US 90713186A US 4661953 A US4661953 A US 4661953A
Authority
US
United States
Prior art keywords
error
data
section
block
combining
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US06/907,131
Inventor
Venkatramiah Venkatesh
Robert M. Maier
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Fujitsu IT Holdings Inc
Original Assignee
Amdahl Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Amdahl Corp filed Critical Amdahl Corp
Priority to US06/907,131 priority Critical patent/US4661953A/en
Application granted granted Critical
Publication of US4661953A publication Critical patent/US4661953A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F11/00Error detection; Error correction; Monitoring
    • G06F11/07Responding to the occurrence of a fault, e.g. fault tolerance
    • G06F11/0703Error or fault processing not based on redundancy, i.e. by taking additional measures to deal with the error or fault not making use of redundancy in operation, in hardware, or in data representation
    • G06F11/0766Error or fault reporting or storing
    • G06F11/0772Means for error signaling, e.g. using interrupts, exception flags, dedicated error registers

Definitions

  • the present invention relates to the field of data processing systems and more particularly to error detection and error location apparatus within data processing systems.
  • the data processing system includes an instruction-controlled principal apparatus and secondary apparatus for independently addressing and accessing points within the principal apparatus.
  • a check-sum generator generates an actual checksum dependent upon the data values of selected points accessed within the principal apparatus. The particular set of points accessed in controlled by the secondary apparatus.
  • the secondary apparatus stores an expected check sum for comparison with the actual checksum. If a comparison indicates that the actual checksum differs from the expected checksum, a fault is indicated within the set of points used in forming the checksum.
  • Recent data processing systems have included diagnostic scanout capabilities which help locate errors in data processing systems.
  • diagnostic scanout capabilities which help locate errors in data processing systems.
  • One such scanout system is described in U.S. Pat. No. 4,244,019 entitled "Data Processing System Including A Program-Executing Primary System” assigned to the same assignee as the present invention.
  • U.S. Pat. No. 4,244,019 provides a mechanism for scanout of all designed locations within a data processing system, independently of the normal data paths of that system. This scanout ability is of significant value in locating errors, and each location which has an error can be examined independently. However, the ability to examine thousands of locations within a data processing system does not assist in a quick location of the errors without further information as to which locations may be the cause of the errors. Although the above error checking and locating techniques have proved useful, there is a need for still improved error checking and locating techniques within data processing systems.
  • the present invention is an error-tracking unit within a data processing system.
  • Each data location to be checked for error and to be located in the case of an error is provided with error detection circuitry.
  • Each data location is additionally provided with an error history register for storing an error signal.
  • the error-detecting circuit detects an error, the error history register is enabled to store the error signal.
  • the error history registers are inhibited from further change so that errors are not propagated.
  • the error detection also causes a machine check signal which, in general, prevents the data processing system from normal processing.
  • the data locations to be error detected and error located are organized into a hierarchy of sets and subsets within the data processing system. In a three-level hierarchy the subsets are named sections, blocks, and units. Each of the data locations in a section have their error detecting signal lines combined and encoded to form a section error signal.
  • the section error signals from a plurality of sections in turn are combined to form a block error signal.
  • a plurality of block error signals are combined to form a unit error signal.
  • groups of error signals from sections, blocks and units are encoded at each level to reduce the number of error signals employed.
  • the error signal Under the condition that a single data location causes an error, the error signal will be propagated through the subsets. For example, a data location error signal will cause a section error signal which in turn will cause a block error signal which in turn will cause a unit error signal.
  • the error signals identify where in the system that the error is located.
  • the unit error signal identifies one of a number of units
  • the block error signal identifies one of a number of blocks in the unit
  • the section error signal identifies one of a number of sections in a block.
  • the present invention freezes the error history registers in the same cycle that an error is detected. In this way, propagation of errors throughout the system is minimized.
  • the grouping and encoding of locations to be checked provides a track which allows the error location to be easily identified.
  • the present invention achieves the objective of providing an improved error detecting and tracking mechanism within a data processing system.
  • FIG. 1 depicts a data processing system organized into units, groups and sections and including an error tracking apparatus.
  • FIG. 2 depicts further details of a typical one of the units of FIG. 1 orginized into blocks.
  • FIG. 3 depicts further details of a typical one of the blocks of FIG. 2 organized into sections.
  • FIG. 4 depicts a schematic representation of the error tracking apparatus of the present invention within one section.
  • FIG. 5 depicts another embodiment of an error tracking apparatus in one section in which the error signals are encoded.
  • FIG. 6 depicts the error tracking apparatus of FIG. 4 in a hierarchy in which section error signals are combined to form block error signals which in turn are combined to form unit error signals.
  • a data processing system 1 includes a number of units 2-1, 2-2, . . . ,2-8.
  • the system 1 is for example a high performance data processing system such as the Amdahl 580 System.
  • an error tracking apparatus 3 is provided for detecting and tracking errors within the units 2-1 thru 2-8.
  • each of the units 2 is formed by a number blocks 4.
  • the blocks typically correspond to the circuit chips on a multi-chip carrier (MCC).
  • MCC multi-chip carrier
  • the unit 2-1 includes MCC's or blocks 4-1, 4-2, . . . ,4-X.
  • Each of the other units 2-2, . . . ,2-8 also includes similar blocks.
  • FIG. 2 a typical ones of the blocks 4-1, . . . ,4-X within the system of FIG.1 are shown.
  • Each block includes sections of which sections 6-1, . . . ,6-Y are typical.
  • the blocks also include block error tracking apparatus 5-1, . . . ,5-X which provide the block error signal lines 29-1, . . . ,29-X, respectively.
  • FIG. 3 typical ones of the sections 6-1, . . . ,6-Y of FIG.2 are shown.
  • Each section includes a number of data locations of which 7-1, 7-2, . . . ,7-Z are typical.
  • the data locations include register locations, memory locations, control locations and other similar locations throughout the data processing system.
  • the sections include the section error-tracking apparatus 24-1, . . . ,24-Y which provide the section error signals 13-1, . . . ,13-Y.
  • FIG. 4 two register locations 7-1 and 7-2, together with the corresponding section error-tracking apparatus 24-1 in a section 6-1 of FIG.3 are shown.
  • the location 7-1 is a 9-bit register representing byte 1.
  • Data location 7-1 is a location within section 6-1, within block 4-1, within unit 2-1 (see FIGS.1, 2 and 3).
  • the output bus 8-1 from the register 7-1 connects, in the FIG. 1 system, to some normal data location (not shown).
  • the output 8-2 from register 7-2 connects on bus 8-2 to some normal location (not shown) in the system of FIG. 1.
  • the registers 7-1 and 7-2 are merely examples of many more data locations 7-1, 7-2, . . . ,7-Z throughout the system of FIG. 1.
  • section error tracking apparatus 24-1 (part of the error tracking apparatus 3 of FIG. 1) includes an error detector.
  • the error detector is a parity checker 9-1 which checks the parity of the data in the register 7-1 and the parity checker 9-2 which checks the parity of the data in register 7-2.
  • the output from checkers 9-1 and 9-2 are asserted if a parity error occurs.
  • Gates 10-1 and 10-2 propagate one of their outputs 20-1 and 20-2 to the OR Gate 12 which asserts a processing damage (PD) signal on line 13-1 if any parity error is detected.
  • the processing damage (PD) signal on line 13-1 is connected to the FIG. 1 system in a conventional manner which, for a typical operation, causes the system to generate a machine check signal.
  • a machine check signal will stop the clocks in one or more of the units of FIG.1 and control will be transferred to the console unit 2-8.
  • the console unit 2-8 is notified of a machine check condition.
  • the console scans the system after the clocks have been stopped to determine the location of the error causing circuit.
  • the console is notified of the machine check condition but the system clocks are not stopped and processing continues.
  • the other outputs from the gates 10-1 and 10-2 connect through the gates 14-1 and 14-2 to the error history registers 11-1 and 11-2, respectively.
  • Gates 14-1, and 14-2 must be enabled by the clock signal, -CS, and the absence of a freeze signal on line 16 from freeze latch 15.
  • the error history registers 11-1 and 11-2 latch any parity error signal generated by the parity checkers 9-1 and 9-2, respectively, when gates 14-1 and 14-2 are enabled. Accordingly, the generation of a parity error signal becomes immediately latched into one of the error history latches 11-1 or 11-2.
  • processing damage signal line 13-1 will cause the clock signals in the system of FIG. 1 to be stopped so that the generation of further errors as a result of the original error is inhibited.
  • the freeze error history (FEH) latch 15 receives an input from all of the gates 14-1, . . . ,14-2 and becomes latched whenever a parity error is detected.
  • the freeze error latch 15 When the freeze error latch 15 is latched, its output on line 16 is input to the gates 14-1 and 14-2 to inhibit any further latching of an error signal into the error history registers 11-1 and 11-2. Accordingly, after the first parity error signal is generated, the gates 14-1 and 14-2 are inhibited from propagating any additional error signals to the error history latches 11-1 and 11-2.
  • the register 17 is a control history register which stores the state of a control signal, CONTROL, on line 18 at the time that any error is detected.
  • An error checker 9-3 detects the control signal on line 18 to detect if there is an error condition.
  • the gate 10-3 propagates any error signal from the error checker 9-3 to the gate 14-3.
  • Another output from gate 10-3 connects to OR gate 30 to provide the system damage (SD) error signal on line 31-1.
  • Gate 14-3 when enabled, like gates 14-1 and 14-2, will cause the freeze error history latch 15 to be set. Also, one output from gate 14-3 latches the control error history signal into the control error history register 19.
  • FIG. 5 a similar and alternate structure to that of FIG. 4 is shown.
  • FIG. 5 differs from FIG. 4 however, in that the error signals on lines 20-1 and 20-2 from the gates 10-1 and 10-2 also connect into an encoder 21.
  • the encoder 21 encodes any error singals on lines 20-1 through 20-Z to provide an N-bit encoded error signal on line 22.
  • the N-Way gate 23 when enabled by the absence of a freeze error output from latch 15 and by the clock signal, propagates the encoded error signal into latch 24.
  • the encoded value encoded by the encoder 21 identifies which one of the registers 7-1, . . . , 7-Z causes the error. While only two registers 7-1 and 7-2 are shown, the three dots (“. . . ") indicate that many registers or other data locations 7-1, . . . ,7-Z are intended.
  • the (scanout) register 24 stores the encoded error representation.
  • Register 24 includes N bits and therefore represents 2 N different error signals. For example, if seven error detectors 9-1, 9-2, . . . ,9-7 exist and seven gates 10-1, 10-2, . . . ,10-7 exist, then Z is equal to 7.
  • Encoder 21 therefore has the seven input lines 21-1, 21-2, . . . ,21-7.
  • the encoder 21 encodes the seven inputs into three lines, that is, N is equal to 3.
  • An all 0's code indicates no error.
  • the gate 23 is three deep, one for each of the lines from encoder 21.
  • the gate 23 provides three inputs to the 3-bit register 24.
  • the error detectors 9-1 through 9-7 are identified by the binary representations 001, . . . ,111.
  • the encoder 21 will encode a binary 010 into the scanout register 24.
  • the 3-bit bus 45 from the scanout register 24 can be interrogated by any conventional scanout circuits.
  • conventional scanout circuits are shown in U.S. Pat. No. 4,244,019 referenced above.
  • An alternate embodiment for multi-bit errors detected in the same cyle can use additional output lines to identify the multi-bit error condition and the location of the errors.
  • the binary number stored in the scanout register 24 is 010, it signifies that the parity error occurred in the data location of register 7-2. If the binary number stored in scanout register 24 is 001, it indicates that the parity error occurred in the register 7-1.
  • freeze error history (FEH) register 15 and scanout register (SO) 24 are each reset by the error reset signal on line 46.
  • FIG. 5 only the processing damage line 13-1 and the scanout bus 45 are shown.
  • the processing damage circuitry of FIG. 5 can be combined with the control error detector and history unit 27 of FIG. 4.
  • the N-bit bus 45 from SO register 24 is only three bits.
  • the encoded scanout output reduces the number of outputs from eight to three.
  • the system includes three groups of circuits, including the section level, the block level, and the unit level.
  • the section level is composed of a plurality of sections. Particularly, the sections 6-1, . . . ,6-Y are each like the section shown in FIG. 4.
  • Each of the sections provides the section error signal lines 13-1, . . . ,13-Y as inputs to one of the blocks in the block level apparatus 5-1.
  • the error signal lines 13-1, . . . ,13-Y are all input to the block 4-X.
  • Block 4-X is typical of blocks 4-1, . . . ,4-X. Each of those blocks receives inputs from a group of sectios like the sections 6-1, . . . ,6-Y.
  • block 4-X is shown in detail as typical.
  • the block 4-X includes an OR gate 34 which receives the section error signal lines 13-1, . . . ,13-Y. Whenever a section error signal occurs, OR gate 34 provides a processing damage signal on output line 29-X. Also, gate 34 provides a latching signal into freeze error history (FEH) register 35. Register 37 is like the register 15 of FIGS.4 and 5. FEH register 35 latches the section error signal unless the clock signal, -CS, through gate 35 is inhibited by the output from FEH register 35.
  • FEH freeze error history
  • encoder 32 encodes Y-inputs 13-1, . . . ,13-Y to form an N-bit output to the N-way gate 33.
  • Gate 33 provides an N-bit bus as an input to the N-bit scanout (SO) register 36.
  • the scanout register 36 is like the scanout register 24 of FIG. 5.
  • the freeze error history latch 35 and the scanout register 36 are reset by the error history reset line 47.
  • Each of the blocks 4-1 through 4-X in FIG. 6 provides a block error signal output.
  • the block error signal lines 29-1, . . . 29-X connect to the unit level tracking apparatus 25-1.
  • the unit tracking apparatus 49 is shown for the unit 2-1 of FIG. 1 and is typical of the unit tracking apparatus of the units 2-1 through 2-8.
  • the OR gate 41 collects the block error signal lines 29-1 through 29-X from the group of blocks 4-1 through 4-X. Whenever any of the block error signal lines signifies an error, OR gate 41 latches the freeze error history (FEH) latch 42, provided the clock signal is enabled by the gate 44.
  • FH freeze error history
  • the encoder 38 encodes the block error signal lines 29-1 through 29-X into an N-bit signal to the N-way gate 39.
  • Gate 39 in turn stores the encoded block error signals into the scanout (SO) register 43. Any error output signal from the OR gate 41 is also latched into the registers 52 and 53 for controlling the processing which can be carried out by the machine check and scanout circuitry.
  • the OR gate 34 Upon the detection of an error by any of the error detection circuits within any of the sections 6-1 through 6-Y, the OR gate 34 will receive a section error signal. The section error signal will be latched into the latch 35 and an encoded representation identifying that error signal is stored in the scanout register 36. The OR gate 34 also causes the OR gate 41 to receive a block error signal which is latched into the FEH latch 42. At the same time, the encoder 38 encodes an identification of that block error signal in the SO register 43.
  • the particular block, for example block 4-X, and the particular section, for example, section 6-1, which caused the error can be identified.
  • no encoder was utilized within the section, and therefore the particular data location, referring to FIG. 4, for the registers 7-1 through 7-X which caused the error is not immediately available. Therefore each of the registers 11-1 through 11-X must be interrogated to see which one caused the error.
  • the FIG. 5 section with an encoder 21 can be employed. Only the scanout register 24 would need interrogation to uniquely identify the data location causing an error.
  • FIG. 6 for clarity, only the processing damage portion of the circuitry is shown at the block and unit levels. However, system damage resulting from control sections like that shown in FIG. 4 can be incorporated in the block and unit levels in the same way that the processing damage sections are shown.
  • the control data locations can be encoded and identified in the same way that the data lines are encoded in the example described.

Landscapes

  • Engineering & Computer Science (AREA)
  • Theoretical Computer Science (AREA)
  • Quality & Reliability (AREA)
  • Physics & Mathematics (AREA)
  • General Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Detection And Correction Of Errors (AREA)

Abstract

Disclosed is an error-tracking unit within a data processing system. Each data location to be checked for error and to be located in the case of an error is provided with error detection circuitry. Each data location is additionally provided with an error history register for storing an error signal. When the error-detecting circuit detects an error, the error history register is enabled to store the error signal. Whenever an error is detected, the error history registers are inhibited from further change so that errors are not propagated. The error detection also causes a machine check signal which, in general, prevents the data processing system from normal processing.

Description

This application is a continuation of U.S. patent application Ser. No. 790,179 filed Dec. 22, 1985, now abandoned, which in turn is a continuation of U.S. patent application, Ser. No. 527,173 filed Aug. 26, 1983, now abandoned.
BACKGROUND OF THE INVENTION
The present invention relates to the field of data processing systems and more particularly to error detection and error location apparatus within data processing systems.
In large data processing systems, the location of the circuits causing errors is a difficult task. One difficulty is that the data changes each cycle of the machine. Once an error is made, the error tends to become propagated to different locations throughout the machine. In each subsequent cycle after the error-causing cycle, the original error frequently causes many more errors. This propagation and proliferation of errors tends to mask the data location which originally caused the error.
One error checking and locating mechanism is described in U.S. Pat. No. 4,132,243, entiled "Data Processing System and Information Scanout Employing Checksums for Error Detection" assigned to same assignee as the present invention.
In that patent, the data processing system includes an instruction-controlled principal apparatus and secondary apparatus for independently addressing and accessing points within the principal apparatus. A check-sum generator generates an actual checksum dependent upon the data values of selected points accessed within the principal apparatus. The particular set of points accessed in controlled by the secondary apparatus. The secondary apparatus stores an expected check sum for comparison with the actual checksum. If a comparison indicates that the actual checksum differs from the expected checksum, a fault is indicated within the set of points used in forming the checksum.
Once a fault has been detected through comparisons of actual and expected check sums, it is possible to further analyze the set of points which entered into the checksum to determine what subset of points is the source of the fault. The set of points or the subset of points accessed to form a checksum is controlled by the secondary apparatus.
While the checksum mechanism of U.S. Pat. No. 4,132,243 has proved very useful, it still has the problem that it requires storage of a large number of expected checksums to reflect the many error-free states of the computer. Furthermore, if improvements and changes to the circuitry and operation of the system mandate that the expected checksums change. Accordingly, keeping track of the expected checksums is somewhat of a burden which is undesirable.
Recent data processing systems have included diagnostic scanout capabilities which help locate errors in data processing systems. One such scanout system is described in U.S. Pat. No. 4,244,019 entitled "Data Processing System Including A Program-Executing Primary System" assigned to the same assignee as the present invention.
U.S. Pat. No. 4,244,019 provides a mechanism for scanout of all designed locations within a data processing system, independently of the normal data paths of that system. This scanout ability is of significant value in locating errors, and each location which has an error can be examined independently. However, the ability to examine thousands of locations within a data processing system does not assist in a quick location of the errors without further information as to which locations may be the cause of the errors. Although the above error checking and locating techniques have proved useful, there is a need for still improved error checking and locating techniques within data processing systems.
SUMMARY OF THE INVENTION
The present invention is an error-tracking unit within a data processing system. Each data location to be checked for error and to be located in the case of an error is provided with error detection circuitry. Each data location is additionally provided with an error history register for storing an error signal. When the error-detecting circuit detects an error, the error history register is enabled to store the error signal. Whenever an error is detected, the error history registers are inhibited from further change so that errors are not propagated. The error detection also causes a machine check signal which, in general, prevents the data processing system from normal processing.
The data locations to be error detected and error located are organized into a hierarchy of sets and subsets within the data processing system. In a three-level hierarchy the subsets are named sections, blocks, and units. Each of the data locations in a section have their error detecting signal lines combined and encoded to form a section error signal. The section error signals from a plurality of sections in turn are combined to form a block error signal. A plurality of block error signals are combined to form a unit error signal.
In one embodiment, groups of error signals from sections, blocks and units are encoded at each level to reduce the number of error signals employed.
Under the condition that a single data location causes an error, the error signal will be propagated through the subsets. For example, a data location error signal will cause a section error signal which in turn will cause a block error signal which in turn will cause a unit error signal. The error signals identify where in the system that the error is located. The unit error signal identifies one of a number of units, the block error signal identifies one of a number of blocks in the unit, and the section error signal identifies one of a number of sections in a block.
The present invention freezes the error history registers in the same cycle that an error is detected. In this way, propagation of errors throughout the system is minimized. The grouping and encoding of locations to be checked provides a track which allows the error location to be easily identified.
In accordance with the above summary, the present invention achieves the objective of providing an improved error detecting and tracking mechanism within a data processing system.
Additional objects and features of the invention will appear from the following description in which the preferred embodiments of the invention have been set forth in detail in conjunction with the drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 depicts a data processing system organized into units, groups and sections and including an error tracking apparatus.
FIG. 2 depicts further details of a typical one of the units of FIG. 1 orginized into blocks.
FIG. 3 depicts further details of a typical one of the blocks of FIG. 2 organized into sections.
FIG. 4 depicts a schematic representation of the error tracking apparatus of the present invention within one section.
FIG. 5 depicts another embodiment of an error tracking apparatus in one section in which the error signals are encoded.
FIG. 6 depicts the error tracking apparatus of FIG. 4 in a hierarchy in which section error signals are combined to form block error signals which in turn are combined to form unit error signals.
DETAILED DESCRIPTION
In FIG. 1, a data processing system 1 includes a number of units 2-1, 2-2, . . . ,2-8. The system 1 is for example a high performance data processing system such as the Amdahl 580 System. In addition to the normal circuits within the system 1, an error tracking apparatus 3 is provided for detecting and tracking errors within the units 2-1 thru 2-8.
In FIG. 1, each of the units 2 is formed by a number blocks 4. For example, the blocks typically correspond to the circuit chips on a multi-chip carrier (MCC). In FIG.1, the unit 2-1 includes MCC's or blocks 4-1, 4-2, . . . ,4-X. Each of the other units 2-2, . . . ,2-8 also includes similar blocks.
In FIG. 2, a typical ones of the blocks 4-1, . . . ,4-X within the system of FIG.1 are shown. Each block includes sections of which sections 6-1, . . . ,6-Y are typical. The blocks also include block error tracking apparatus 5-1, . . . ,5-X which provide the block error signal lines 29-1, . . . ,29-X, respectively.
In FIG. 3, typical ones of the sections 6-1, . . . ,6-Y of FIG.2 are shown. Each section includes a number of data locations of which 7-1, 7-2, . . . ,7-Z are typical. The data locations include register locations, memory locations, control locations and other similar locations throughout the data processing system. The sections include the section error-tracking apparatus 24-1, . . . ,24-Y which provide the section error signals 13-1, . . . ,13-Y.
In FIG. 4, two register locations 7-1 and 7-2, together with the corresponding section error-tracking apparatus 24-1 in a section 6-1 of FIG.3 are shown. In FIG. 4, the location 7-1 is a 9-bit register representing byte 1. Data location 7-1 is a location within section 6-1, within block 4-1, within unit 2-1 (see FIGS.1, 2 and 3). The output bus 8-1 from the register 7-1 connects, in the FIG. 1 system, to some normal data location (not shown). In a similar manner, the output 8-2 from register 7-2 connects on bus 8-2 to some normal location (not shown) in the system of FIG. 1.
The registers 7-1 and 7-2 are merely examples of many more data locations 7-1, 7-2, . . . ,7-Z throughout the system of FIG. 1.
In FIG. 4, section error tracking apparatus 24-1 (part of the error tracking apparatus 3 of FIG. 1) includes an error detector. In the FIG. 4 example, the error detector is a parity checker 9-1 which checks the parity of the data in the register 7-1 and the parity checker 9-2 which checks the parity of the data in register 7-2. The output from checkers 9-1 and 9-2 are asserted if a parity error occurs. Gates 10-1 and 10-2 propagate one of their outputs 20-1 and 20-2 to the OR Gate 12 which asserts a processing damage (PD) signal on line 13-1 if any parity error is detected. The processing damage (PD) signal on line 13-1 is connected to the FIG. 1 system in a conventional manner which, for a typical operation, causes the system to generate a machine check signal.
In the usual operation, a machine check signal will stop the clocks in one or more of the units of FIG.1 and control will be transferred to the console unit 2-8. Typically, the console unit 2-8 is notified of a machine check condition.
In one mode of operation, the console scans the system after the clocks have been stopped to determine the location of the error causing circuit. In another mode of operation, the console is notified of the machine check condition but the system clocks are not stopped and processing continues. These scanning functions are similar to those described in U.S. Pat. Nos. 4,244,019 and 4,142 243 referenced above.
In FIG. 4, the other outputs from the gates 10-1 and 10-2 connect through the gates 14-1 and 14-2 to the error history registers 11-1 and 11-2, respectively. Gates 14-1, and 14-2 must be enabled by the clock signal, -CS, and the absence of a freeze signal on line 16 from freeze latch 15. The error history registers 11-1 and 11-2 latch any parity error signal generated by the parity checkers 9-1 and 9-2, respectively, when gates 14-1 and 14-2 are enabled. Accordingly, the generation of a parity error signal becomes immediately latched into one of the error history latches 11-1 or 11-2. At the same time, processing damage signal line 13-1 will cause the clock signals in the system of FIG. 1 to be stopped so that the generation of further errors as a result of the original error is inhibited.
The freeze error history (FEH) latch 15 receives an input from all of the gates 14-1, . . . ,14-2 and becomes latched whenever a parity error is detected. When the freeze error latch 15 is latched, its output on line 16 is input to the gates 14-1 and 14-2 to inhibit any further latching of an error signal into the error history registers 11-1 and 11-2. Accordingly, after the first parity error signal is generated, the gates 14-1 and 14-2 are inhibited from propagating any additional error signals to the error history latches 11-1 and 11-2. In FIG. 4, the register 17 is a control history register which stores the state of a control signal, CONTROL, on line 18 at the time that any error is detected. An error checker 9-3 detects the control signal on line 18 to detect if there is an error condition. The gate 10-3 propagates any error signal from the error checker 9-3 to the gate 14-3. Another output from gate 10-3 connects to OR gate 30 to provide the system damage (SD) error signal on line 31-1. Gate 14-3 when enabled, like gates 14-1 and 14-2, will cause the freeze error history latch 15 to be set. Also, one output from gate 14-3 latches the control error history signal into the control error history register 19.
In FIG. 5, a similar and alternate structure to that of FIG. 4 is shown. FIG. 5 differs from FIG. 4 however, in that the error signals on lines 20-1 and 20-2 from the gates 10-1 and 10-2 also connect into an encoder 21. The encoder 21 encodes any error singals on lines 20-1 through 20-Z to provide an N-bit encoded error signal on line 22. The N-Way gate 23, when enabled by the absence of a freeze error output from latch 15 and by the clock signal, propagates the encoded error signal into latch 24. The encoded value encoded by the encoder 21 identifies which one of the registers 7-1, . . . , 7-Z causes the error. While only two registers 7-1 and 7-2 are shown, the three dots (". . . ") indicate that many registers or other data locations 7-1, . . . ,7-Z are intended.
In FIG. 5, the (scanout) register 24 stores the encoded error representation. Register 24 includes N bits and therefore represents 2N different error signals. For example, if seven error detectors 9-1, 9-2, . . . ,9-7 exist and seven gates 10-1, 10-2, . . . ,10-7 exist, then Z is equal to 7. Encoder 21 therefore has the seven input lines 21-1, 21-2, . . . ,21-7. The encoder 21 encodes the seven inputs into three lines, that is, N is equal to 3. An all 0's code indicates no error. The gate 23 is three deep, one for each of the lines from encoder 21. The gate 23 provides three inputs to the 3-bit register 24. For a binary representation, the error detectors 9-1 through 9-7 are identified by the binary representations 001, . . . ,111. In an example where the parity detector 9-2 detects a parity error in the data in data location 7-2, the encoder 21 will encode a binary 010 into the scanout register 24. The 3-bit bus 45 from the scanout register 24 can be interrogated by any conventional scanout circuits. For example, conventional scanout circuits are shown in U.S. Pat. No. 4,244,019 referenced above.
An alternate embodiment for multi-bit errors detected in the same cyle can use additional output lines to identify the multi-bit error condition and the location of the errors.
If the binary number stored in the scanout register 24 is 010, it signifies that the parity error occurred in the data location of register 7-2. If the binary number stored in scanout register 24 is 001, it indicates that the parity error occurred in the register 7-1.
In FIG. 5, the freeze error history (FEH) register 15 and scanout register (SO) 24 are each reset by the error reset signal on line 46.
In FIG. 5, only the processing damage line 13-1 and the scanout bus 45 are shown.
The processing damage circuitry of FIG. 5 can be combined with the control error detector and history unit 27 of FIG. 4. In comparing the FIG. 4 and FIG. 5 implementation, note that the N-bit bus 45 from SO register 24 is only three bits. By way of distribution, in the FIG. 4 embodiedment, there is an output from each of the eight registers 11-1, 11-2, . . . ,11-8 in a comparable example. The encoded scanout output reduces the number of outputs from eight to three.
In FIG. 6, further details of the error tracking hierarchy are shown. The system includes three groups of circuits, including the section level, the block level, and the unit level. The section level is composed of a plurality of sections. Particularly, the sections 6-1, . . . ,6-Y are each like the section shown in FIG. 4. Each of the sections provides the section error signal lines 13-1, . . . ,13-Y as inputs to one of the blocks in the block level apparatus 5-1. The example shown, the error signal lines 13-1, . . . ,13-Y are all input to the block 4-X. Block 4-X is typical of blocks 4-1, . . . ,4-X. Each of those blocks receives inputs from a group of sectios like the sections 6-1, . . . ,6-Y.
In FIG. 6, block 4-X is shown in detail as typical. The block 4-X includes an OR gate 34 which receives the section error signal lines 13-1, . . . ,13-Y. Whenever a section error signal occurs, OR gate 34 provides a processing damage signal on output line 29-X. Also, gate 34 provides a latching signal into freeze error history (FEH) register 35. Register 37 is like the register 15 of FIGS.4 and 5. FEH register 35 latches the section error signal unless the clock signal, -CS, through gate 35 is inhibited by the output from FEH register 35.
In FIG. 6, encoder 32 encodes Y-inputs 13-1, . . . ,13-Y to form an N-bit output to the N-way gate 33. Gate 33 provides an N-bit bus as an input to the N-bit scanout (SO) register 36. The scanout register 36 is like the scanout register 24 of FIG. 5. The freeze error history latch 35 and the scanout register 36 are reset by the error history reset line 47.
Each of the blocks 4-1 through 4-X in FIG. 6 provides a block error signal output. The block error signal lines 29-1, . . . 29-X connect to the unit level tracking apparatus 25-1.
In FIG. 6, the unit tracking apparatus 49 is shown for the unit 2-1 of FIG. 1 and is typical of the unit tracking apparatus of the units 2-1 through 2-8.
In FIG. 6, the OR gate 41 collects the block error signal lines 29-1 through 29-X from the group of blocks 4-1 through 4-X. Whenever any of the block error signal lines signifies an error, OR gate 41 latches the freeze error history (FEH) latch 42, provided the clock signal is enabled by the gate 44.
In FIG. 6, the encoder 38 encodes the block error signal lines 29-1 through 29-X into an N-bit signal to the N-way gate 39. Gate 39 in turn stores the encoded block error signals into the scanout (SO) register 43. Any error output signal from the OR gate 41 is also latched into the registers 52 and 53 for controlling the processing which can be carried out by the machine check and scanout circuitry.
The operation of the FIG. 6 apparatus is as follows. Upon the detection of an error by any of the error detection circuits within any of the sections 6-1 through 6-Y, the OR gate 34 will receive a section error signal. The section error signal will be latched into the latch 35 and an encoded representation identifying that error signal is stored in the scanout register 36. The OR gate 34 also causes the OR gate 41 to receive a block error signal which is latched into the FEH latch 42. At the same time, the encoder 38 encodes an identification of that block error signal in the SO register 43.
By interrogating (for example, with scanout circuitry) the SO register 43 and the SO register 36, the particular block, for example block 4-X, and the particular section, for example, section 6-1, which caused the error can be identified. In the FIG. 6 example, no encoder was utilized within the section, and therefore the particular data location, referring to FIG. 4, for the registers 7-1 through 7-X which caused the error is not immediately available. Therefore each of the registers 11-1 through 11-X must be interrogated to see which one caused the error. In an alternate embodiment, the FIG. 5 section with an encoder 21 can be employed. Only the scanout register 24 would need interrogation to uniquely identify the data location causing an error.
In the FIG. 6 description, for clarity, only the processing damage portion of the circuitry is shown at the block and unit levels. However, system damage resulting from control sections like that shown in FIG. 4 can be incorporated in the block and unit levels in the same way that the processing damage sections are shown. The control data locations can be encoded and identified in the same way that the data lines are encoded in the example described.
While the invention has been particularly shown and described with reference to preferred embodiments thereof, it will be understood by those skilled in the art that the foregoing and other changes in form and detail may be made therein without departing from the spirit and scope of the invention.

Claims (6)

What is claimed is:
1. In a data processing system including a plurality of data locations, an error tracking apparatus comprising:
a plurality of error detection means, each for detecting errors in data locations, and generating a data error signal upon the occurrence of an error;
a plurality of storage means, each connected to store a data error signal from a corresponding data location upon the detection of an error and adapted to be read during error processing;
an error freeze latch connected to be set by a data error signal generated by said error detection means, said error freeze latch connected to inhibit said storage means from changing state after being set by the data error signal;
a first combining means for combining the error signals from a section of said data locations to form a section error signal representing an error in any of said data locations within said section; and
a second combining means for combining a block of said section error signals to form a block error signal indicating an error in a data location within said block of sections, whereby the block and section of the data location causing the error is identified.
2. The apparatus of claim 1 wherein said storage means includes means to store the data error signal in the same cycle as the error is detected.
3. The apparatus of claim 1 including scanout means connected to distribute data error signals stored in said storage means for error processing.
4. The apparatus of claim 1 further including third combining means for combining a plurality of block error signals from a group of blocks to form a unit error signal indicating an error in a data location within said group of blocks whereby the unit, block and section of the data location causing the error is identified.
5. The apparatus of claim 4 wherein said third combining means for combining a plurality of said block error signals includes an encoder to provide an encoded representation of said block error signals.
6. The apparatus of claim 4 wherein said first combining means for combining the error signal from a group of said data locations includes an encoder means for encoding said section error signals to form an encoded representation of said section error signals.
US06/907,131 1985-10-22 1986-09-12 Error tracking apparatus in a data processing system Expired - Lifetime US4661953A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US06/907,131 US4661953A (en) 1985-10-22 1986-09-12 Error tracking apparatus in a data processing system

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US79017985A 1985-10-22 1985-10-22
US06/907,131 US4661953A (en) 1985-10-22 1986-09-12 Error tracking apparatus in a data processing system

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
US79017985A Continuation 1985-10-22 1985-10-22

Publications (1)

Publication Number Publication Date
US4661953A true US4661953A (en) 1987-04-28

Family

ID=27121003

Family Applications (1)

Application Number Title Priority Date Filing Date
US06/907,131 Expired - Lifetime US4661953A (en) 1985-10-22 1986-09-12 Error tracking apparatus in a data processing system

Country Status (1)

Country Link
US (1) US4661953A (en)

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4755997A (en) * 1985-10-03 1988-07-05 Mitsubishi Denki Kabushiki Kaisha Computer program debugging system
US4769761A (en) * 1986-10-09 1988-09-06 International Business Machines Corporation Apparatus and method for isolating and predicting errors in a local area network
US4866712A (en) * 1988-02-19 1989-09-12 Bell Communications Research, Inc. Methods and apparatus for fault recovery
US4924466A (en) * 1988-06-30 1990-05-08 International Business Machines Corp. Direct hardware error identification method and apparatus for error recovery in pipelined processing areas of a computer system
US4992978A (en) * 1988-03-31 1991-02-12 Wiltron Company Cross-path optimization in multi-task processing
US4996688A (en) * 1988-09-19 1991-02-26 Unisys Corporation Fault capture/fault injection system
US5063535A (en) * 1988-11-16 1991-11-05 Xerox Corporation Programming conflict identification system for reproduction machines
US5146586A (en) * 1989-02-17 1992-09-08 Nec Corporation Arrangement for storing an execution history in an information processing unit
US5163051A (en) * 1990-02-02 1992-11-10 Telecom Analysis Systems Inc. Paired bit error rate tester
US5383201A (en) * 1991-12-23 1995-01-17 Amdahl Corporation Method and apparatus for locating source of error in high-speed synchronous systems
US5448725A (en) * 1991-07-25 1995-09-05 International Business Machines Corporation Apparatus and method for error detection and fault isolation
US5490250A (en) * 1991-12-31 1996-02-06 Amdahl Corporation Method and apparatus for transferring indication of control error into data path of data switcher
US5680404A (en) * 1992-03-31 1997-10-21 Mitel Corporation Cycling error count for link maintenance
WO2001016746A2 (en) * 1999-08-31 2001-03-08 Sun Microsystems, Inc. Method and apparatus for extracting first failure and attendant operating information from computer system devices
US20040267947A1 (en) * 2003-06-24 2004-12-30 Sheahan Thomas J. System and method for communicating with an appliance through an optical interface using a control panel indicator
US20080126830A1 (en) * 2006-09-16 2008-05-29 International Business Machines Corporation Error accumulation register, error accumulation method, and error accumulation system
US20080209291A1 (en) * 2007-02-27 2008-08-28 Advanced Micro Devices, Inc. Over temperature detection apparatus and method thereof
US20090125760A1 (en) * 2004-11-19 2009-05-14 Kw-Software Gmbh Method and apparatus for safe parameterization in accordance with IEC 61508 SIL 1 to 3 or EN 954-1 Categories 1 to 4

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3704363A (en) * 1971-06-09 1972-11-28 Ibm Statistical and environmental data logging system for data processing storage subsystem
US3838260A (en) * 1973-01-22 1974-09-24 Xerox Corp Microprogrammable control memory diagnostic system
US3906200A (en) * 1974-07-05 1975-09-16 Sperry Rand Corp Error logging in semiconductor storage units
US3917933A (en) * 1974-12-17 1975-11-04 Sperry Rand Corp Error logging in LSI memory storage units using FIFO memory of LSI shift registers
US4062061A (en) * 1976-04-15 1977-12-06 Xerox Corporation Error log for electrostatographic machines
US4453213A (en) * 1981-07-30 1984-06-05 Harris Corporation Error reporting scheme
US4454583A (en) * 1981-06-30 1984-06-12 Signal Scanning Products, Inc. Navigation system
US4456994A (en) * 1979-01-31 1984-06-26 U.S. Philips Corporation Remote simulation by remote control from a computer desk
US4497057A (en) * 1981-08-07 1985-01-29 Nippondenso Co., Ltd. Motor vehicle diagnostic monitoring system
US4499581A (en) * 1982-09-21 1985-02-12 Xerox Corporation Self testing system for reproduction machine

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3704363A (en) * 1971-06-09 1972-11-28 Ibm Statistical and environmental data logging system for data processing storage subsystem
US3838260A (en) * 1973-01-22 1974-09-24 Xerox Corp Microprogrammable control memory diagnostic system
US3906200A (en) * 1974-07-05 1975-09-16 Sperry Rand Corp Error logging in semiconductor storage units
US3917933A (en) * 1974-12-17 1975-11-04 Sperry Rand Corp Error logging in LSI memory storage units using FIFO memory of LSI shift registers
US4062061A (en) * 1976-04-15 1977-12-06 Xerox Corporation Error log for electrostatographic machines
US4456994A (en) * 1979-01-31 1984-06-26 U.S. Philips Corporation Remote simulation by remote control from a computer desk
US4454583A (en) * 1981-06-30 1984-06-12 Signal Scanning Products, Inc. Navigation system
US4453213A (en) * 1981-07-30 1984-06-05 Harris Corporation Error reporting scheme
US4497057A (en) * 1981-08-07 1985-01-29 Nippondenso Co., Ltd. Motor vehicle diagnostic monitoring system
US4499581A (en) * 1982-09-21 1985-02-12 Xerox Corporation Self testing system for reproduction machine

Cited By (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4755997A (en) * 1985-10-03 1988-07-05 Mitsubishi Denki Kabushiki Kaisha Computer program debugging system
US4769761A (en) * 1986-10-09 1988-09-06 International Business Machines Corporation Apparatus and method for isolating and predicting errors in a local area network
US4866712A (en) * 1988-02-19 1989-09-12 Bell Communications Research, Inc. Methods and apparatus for fault recovery
US4992978A (en) * 1988-03-31 1991-02-12 Wiltron Company Cross-path optimization in multi-task processing
US4924466A (en) * 1988-06-30 1990-05-08 International Business Machines Corp. Direct hardware error identification method and apparatus for error recovery in pipelined processing areas of a computer system
US4996688A (en) * 1988-09-19 1991-02-26 Unisys Corporation Fault capture/fault injection system
US5063535A (en) * 1988-11-16 1991-11-05 Xerox Corporation Programming conflict identification system for reproduction machines
US5146586A (en) * 1989-02-17 1992-09-08 Nec Corporation Arrangement for storing an execution history in an information processing unit
US5163051A (en) * 1990-02-02 1992-11-10 Telecom Analysis Systems Inc. Paired bit error rate tester
US5448725A (en) * 1991-07-25 1995-09-05 International Business Machines Corporation Apparatus and method for error detection and fault isolation
US5383201A (en) * 1991-12-23 1995-01-17 Amdahl Corporation Method and apparatus for locating source of error in high-speed synchronous systems
US5490250A (en) * 1991-12-31 1996-02-06 Amdahl Corporation Method and apparatus for transferring indication of control error into data path of data switcher
US5680404A (en) * 1992-03-31 1997-10-21 Mitel Corporation Cycling error count for link maintenance
WO2001016746A2 (en) * 1999-08-31 2001-03-08 Sun Microsystems, Inc. Method and apparatus for extracting first failure and attendant operating information from computer system devices
WO2001016746A3 (en) * 1999-08-31 2001-10-04 Sun Microsystems Inc Method and apparatus for extracting first failure and attendant operating information from computer system devices
US6499113B1 (en) 1999-08-31 2002-12-24 Sun Microsystems, Inc. Method and apparatus for extracting first failure and attendant operating information from computer system devices
US20040267947A1 (en) * 2003-06-24 2004-12-30 Sheahan Thomas J. System and method for communicating with an appliance through an optical interface using a control panel indicator
US7243174B2 (en) 2003-06-24 2007-07-10 Emerson Electric Co. System and method for communicating with an appliance through an optical interface using a control panel indicator
US20090125760A1 (en) * 2004-11-19 2009-05-14 Kw-Software Gmbh Method and apparatus for safe parameterization in accordance with IEC 61508 SIL 1 to 3 or EN 954-1 Categories 1 to 4
US7912990B2 (en) * 2004-11-19 2011-03-22 Kw-Software Gmbh Method and apparatus for safe parameterization in accordance with IEC 61508 SIL 1 to 3 or EN 954-1 categories 1 to 4
US20080126830A1 (en) * 2006-09-16 2008-05-29 International Business Machines Corporation Error accumulation register, error accumulation method, and error accumulation system
US7805634B2 (en) * 2006-09-16 2010-09-28 International Business Machines Corporation Error accumulation register, error accumulation method, and error accumulation system
US20080209291A1 (en) * 2007-02-27 2008-08-28 Advanced Micro Devices, Inc. Over temperature detection apparatus and method thereof
US7650550B2 (en) * 2007-02-27 2010-01-19 Globalfoundries Inc. Over temperature detection apparatus and method thereof

Similar Documents

Publication Publication Date Title
US4661953A (en) Error tracking apparatus in a data processing system
US6009548A (en) Error correcting code retrofit method and apparatus for multiple memory configurations
US4996688A (en) Fault capture/fault injection system
EP0030612B1 (en) Method of correcting double errors in a data storage apparatus and data storage apparatus
EP0265639A2 (en) ECC circuit failure verifier
CA1315409C (en) Memory diagnostic apparatus and method
US4201337A (en) Data processing system having error detection and correction circuits
US4679195A (en) Error tracking apparatus in a data processing system
JPS58179982A (en) Multi-level cash system
EP0242595B1 (en) Error detection using variable field parity checking
US5953265A (en) Memory having error detection and correction
EP0383899B1 (en) Failure detection for partial write operations for memories
EP1116114B1 (en) Technique for detecting memory part failures and single, double, and triple bit errors
EP0463573A2 (en) Efficient error detection in a VLSI central processing unit
US5491702A (en) Apparatus for detecting any single bit error, detecting any two bit error, and detecting any three or four bit error in a group of four bits for a 25- or 64-bit data word
KR20020020734A (en) A system and method for improving multi-bit error protection in computer memory systems
CA1208795A (en) Data processing scan-art system
EP0084460B1 (en) Improvements in and relating to computer memory control systems
US4205301A (en) Error detecting system for integrated circuit
US4761783A (en) Apparatus and method for reporting occurrences of errors in signals stored in a data processor
US4224681A (en) Parity processing in arithmetic operations
US4035766A (en) Error-checking scheme
EP0319183B1 (en) Parity regeneration self-checking
EP0436123A2 (en) Interrupt generating for single-bit memory errors
US5048024A (en) Partitioned parity check and regeneration circuit

Legal Events

Date Code Title Description
STCF Information on status: patent grant

Free format text: PATENTED CASE

FPAY Fee payment

Year of fee payment: 4

FEPP Fee payment procedure

Free format text: PAYOR NUMBER ASSIGNED (ORIGINAL EVENT CODE: ASPN); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY

FPAY Fee payment

Year of fee payment: 8

FPAY Fee payment

Year of fee payment: 12

FEPP Fee payment procedure

Free format text: PAYER NUMBER DE-ASSIGNED (ORIGINAL EVENT CODE: RMPN); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY

Free format text: PAYOR NUMBER ASSIGNED (ORIGINAL EVENT CODE: ASPN); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY